Methods and systems for mass distribution of supply packs

ABSTRACT

An aerial distribution system and method for deploying items is disclosed. The system includes a box, a lid detachably coupled to the box, a plurality of items within the box, a flexible liner coupled to the box and containing the plurality of items, and at least one strap coupling the lid to the flexible liner. During deployment of the aerial distribution system, air drag removes the lid from the box and inverts the flexible liner to eject the plurality of items from the box.

CROSS REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. Non-Provisional applicationSer. No. 16/151002, filed Oct. 3, 2018, which is a continuation of U.S.Non-Provisional application Ser. No. 14/801250, filed Jul. 16, 2015,which claims priority to U.S. Provisional Application No. 62/025,226,filed Jul. 16, 2014, and U.S. Provisional Application No. 62/091,169,filed Dec. 12, 2014, all entitled “Methods and Systems for MassDistribution of Supply Packs.” The entire disclosures of which arehereby incorporated herein by reference.

BACKGROUND 1. Field of the Invention

The present invention relates to aerial deployment of items. Moreparticularly, the invention is directed to an aerial disbursement systemof items to people on the ground.

2. Description of the Background

Numerous circumstances require the transport and delivery of variouskinds of cargo to inaccessible or remote areas where groundtransportation is not possible or timely. For example, in the event thatpeople are trapped or disabled in a remote area, a hostile environment,or an area ravaged by a natural disaster, it may become necessary ordesirable to supply them with food, water, medicine, shelter, and othersupplies as rapidly as possible. Similarly, in times of warfare,battlefields may be in remote locations or hostile environments.Likewise, it may be necessary to deliver supplies such as fuel tostranded people. Of course, in times of war or other hostilities, it maybe essential to provide support to permit the stranded personnel toevacuate the position in which they find themselves.

Many remote locations or hostile environments may be in areas such asdeserts or large expanses of otherwise uninhabited or inhospitableterrain. Because of the remoteness of a location or its inaccessibility,supplies are often delivered by air drops from airplanes or helicopters.In the event of natural disasters and other emergencies, time may be ofthe essence to deliver sustenance, medicine, or other critical items topeople cut off from life-sustaining supplies. For example, it might beessential to provide water to people cut off from a clean water supplyin the event of flooding, an earthquake, and/or a hurricane.

While in an emergency, the cost of packaging and delivering supplies tothose in need may be considered secondary, it is nevertheless importantto provide packaging for the supplies that can be formed and distributedon a reasonably cost-effective basis. Also, the space taken up by thecontainers or packages, as well as the amount and cost of material fromwhich the containers are fabricated, should be minimized to increase thecost effectiveness thereof.

In the past, relief supplies have been delivered by dropping pallets ofsupplies by parachutes connected to containers. Typically, large amountsof supplies are stacked on multiple pallets and parachutes are connectedto the pallets. However, parachutes are expensive and are typically notrecoverable. Moreover, the parachutes may be quite large and cumbersome.The size of the parachutes depends on the particular supplies to bedistributed. If the parachutes are undersized, the containers descend ata rapid rate and the container may be ruptured and the contents thereoflost, or people on the ground may be harmed by the rapidly-descendingcontainers. Furthermore, if the supplies are stacked together on apallet and the pallet air drop is off target, the supplies may beunrecoverable by those in need. Even if the pallet of supplies isrecoverable, bandits or guerillas have been known to hoard the suppliesand either keep them from people in need or ransom the supplies.

There is a continuing need for a cost-effective package for emergencysupplies that may be easily air dropped and distributed to a largenumber of people with a minimized risk of damage to the supplies andharm to the people collecting the supplies. Additionally, there is acontinuing need for a method and system for manufacturing the packages.

SUMMARY OF THE INVENTION

In concordance with the instant disclosure, an aerial distributionsystem has surprisingly been discovered.

An embodiment of the invention is directed to an aerial distributionsystem for deploying items. The system comprises a box, a lid detachablycoupled to the box, a plurality of items within the box, a flexibleliner coupled to the box and containing the plurality of items and atleast one strap coupling the lid to the flexible liner. Duringdeployment of the aerial distribution system, air drag removes the lidfrom the box and inverts the flexible liner to eject the plurality ofitems from the box.

Preferably, the system further comprises a breakaway bottom of the boxcoupled to the flexible liner, wherein during deployment, breakawaybottom is forced through the box and assists in ejecting the pluralityof items from the box. The flexible liner is preferably coupled to thebox along an upper edge of the box. Preferably, the plurality of itemsare aerodynamic supply packs. In a preferred embodiment, there are fourstraps coupling the lid to the flexible liner. Each strap is preferablycoupled to a corner of the lid and a central portion of the flexibleliner. The system preferably further comprises a reinforcementpositioned at the central portion of the flexible liner.

Another embodiment of the invention is directed to a method of deployingcargo from a vehicle. The method comprises the steps of inserting aflexible liner into a box, coupling at least one strap to the flexibleliner, loading a plurality of items into the flexible liner, couplingthe at least on strap to a lid, covering the box with the lid, loadingthe box into the vehicle, maneuvering the vehicle to a location ofdeployment, and expelling the box from the vehicle, wherein duringdeployment, air drag removes the lid from the box and inverts theflexible liner to eject the plurality of items from the box.

Preferably, the method further comprises coupling a breakaway bottom tothe box and to the flexible liner, wherein during deployment, breakawaybottom is forced through the box and assists in ejecting the pluralityof items from the box. The flexible liner is preferably coupled to thebox along an upper edge of the box. Preferably, the plurality of itemsare aerodynamic supply packs. There are preferably four straps couplingthe lid to the flexible liner. Each strap is preferably coupled to acorner of the lid and a central portion of the flexible liner. In apreferred embodiment, the method further comprises a reinforcementpositioned at the central portion of the flexible liner.

Another embodiment of the invention is directed to an aerialdistribution container. The container comprises a box, a lid detachablycoupled to the box, a flexible liner coupled to the box, and at leastone strap coupling the lid to the flexible liner. During deployment ofthe aerial distribution system, air drag removes the lid from the boxand inverts the flexible liner.

Preferably, the container further comprises a breakaway bottom of thebox coupled to the flexible liner, wherein during deployment, breakawaybottom is forced through the box. The flexible liner is preferablycoupled to the box along an upper edge of the box. Preferably, there arefour straps coupling the lid to the flexible liner. Each strap ispreferably coupled to a corner of the lid and a central portion of theflexible liner. Preferably the container, further comprises areinforcement positioned at the central portion of the flexible liner.

Other embodiments and advantages of the invention are set forth in partin the description, which follows, and in part, may be obvious from thisdescription, or may be learned from the practice of the invention.

DESCRIPTION OF THE DRAWINGS

FIG. 1 is a top perspective view of an emergency pack according to oneembodiment of the disclosure, the emergency pack shown in a formedposition.

FIG. 2 is a bottom perspective view of the emergency pack illustrated inFIG. 1, the emergency pack shown in a formed position.

FIG. 3 is a top perspective view of the emergency pack illustrated inFIGS. 1-2, the emergency pack shown in a flight position.

FIG. 4 is a bottom perspective view of the emergency pack illustrated inFIGS. 1-3, the emergency pack shown in a flight position.

FIG. 5 is a cross-sectional front elevational view of the emergency packtaken at section line A-A in FIG. 3.

FIG. 6 is a fragmentary enlarged cross-sectional front elevational viewof the emergency pack taken at callout B in FIG. 5, further showing aninner package of the emergency pack.

FIG. 7 is a fragmentary enlarged cross-sectional front elevational viewof the emergency pack taken at callout C in FIG. 5, further showing awing of the emergency pack.

FIG. 8 is a fragmentary enlarged cross-sectional front elevational viewof the emergency pack taken at callout D in FIG. 5, further showing arigid insert in an outer package of the emergency pack.

FIG. 9 a cross-sectional side elevational view of the emergency packtaken at section line E-E in FIG. 4, further showing an inner package ofthe emergency pack connected with an outer package of the emergency packaccording to one embodiment of the disclosure, the inner package shownwith a liquid material disposed therein.

FIG. 10 is a cross-sectional side elevational view of the emergency packtaken at section line E-E in FIG. 4, the inner package of the emergencypack shown consisting of a solid material.

FIG. 11 is a side perspective view of a system for producing anemergency pack.

FIG. 12 is an enlarged fragmentary side perspective view of the systemidentified by callout 12 in FIG. 11, further showing a product loadingunit of the system.

FIG. 13 is an enlarged fragmentary side perspective view of the systemidentified by callout 13 in FIG. 11, further showing a longitudinalmid-pack and edge sealing unit and a transverse heat seal unit of thesystem.

FIG. 14 is an enlarged fragmentary side perspective view of the systemidentified by callout 14 in FIG. 11, further showing a perforator unitof the system with an outer cover removed to show a perforating rollerand an anvil roller of the perforator unit.

FIG. 15 is an enlarged fragmentary side perspective view of the systemidentified by callout 15 in FIG. 11, further showing a wing folding unitof the system, an emergency pack removed from the wing folding unit toshow a guide plate of the wing folding unit;

FIG. 16 is an enlarged fragmentary side perspective view of the systemidentified by callout 16 in FIG. 11, further showing a wing band sealingunit of the system.

FIG. 17 is an enlarged fragmentary side perspective view of the systemidentified by callout 17 in FIG. 11, further showing a package separatorunit of the system with an outer cover removed to show a guillotine ofthe package separator unit.

FIG. 18 is an embodiment of the pack having a tail.

FIG. 19 is an embodiment of the pack having vent slits.

FIG. 20 is an embodiment of the pack having scalloped edges.

FIG. 21 is an embodiment of the pack having holes in the wings.

FIG. 22 is an embodiment of the pack having a reinforcing instructioninsert sheet.

FIG. 23 is an embodiment of the pack having an evenly distributedpayload.

FIG. 24 is an embodiment of the pack having perforations for creatinghandles.

FIG. 25 depicts the formation of the wings.

FIGS. 26-28 depict embodiments of the pack having air vents.

FIGS. 29a-b are views of an embodiment of a storage and deploymentcontainer.

FIGS. 30a-c depicts an embodiment of a storage and deployment containerwith a canopy.

FIGS. 31a-d depict an embodiment of a storage and deployment containerwith a staggered slot in the bottom surface.

FIG. 32a-b depict an embodiment of a storage and deployment containerwhere the upper surface opens into a chute.

FIG. 33 depicts an embodiment of a deployment hopper.

FIGS. 34a-c depict an embodiment of a deployment cart.

FIGS. 35a-b depict an embodiment of a deflection device.

FIGS. 36a-b depict an embodiment of a disbursement device.

FIG. 37 depicts another embodiment of a disbursement device.

FIG. 38 depicts an embodiment of a container divider.

FIGS. 39a-c depict an embodiment of a storage and deployment bag.

FIGS. 40a-c depict an embodiment of a gaylord box.

FIG. 41 depicts another embodiment of a gaylord box.

FIG. 42 depicts an embodiment of a deployment system.

FIGS. 43a-f depict another embodiment of a storage and deploymentcontainer.

FIGS. 44a-b depict an embodiment of a pallet.

FIG. 45 depicts an embodiment of an exploded view of a loaded gaylordbox.

FIG. 46 depicts the underside of an embodiment of a gaylord box coupledto a pallet.

FIG. 47 depicts an embodiment of the progress of the gaylord box afterdeployment.

FIGS. 48a-d depict embodiments of boxes with hook and loop strapping.

FIGS. 49a-b depict an embodiment of a box with the lid used to slow thedecent of the box.

FIG. 50a-f depict an embodiment of a deployment device.

DESCRIPTION OF THE INVENTION

Providing supplies to a population under emergency conditions is anextremely risky undertaking. Typically, transportation infrastructureshave been disrupted, for example, by natural disasters or political orsocial upheaval. It is often difficult or impossible to truck reliefsupplies to the disaster area because roads are destroyed and/or accesspoints are blocked. In addition, the relief workers themselves areplaced in danger, which may be from environmental concerns (e.g. floods,mudslides, earthquakes, radiation) or dangerous military actions on theground. Providing supplies by air is often the only viable option in adisaster, but there are still many problems. Because supplies areprovided in bulk, the process generally requires precise targeting andcoordination with those on the ground to avoid damage to the suppliesthemselves, damage to structures on the ground, and harm to persons andanimals. Whether delivered by truck, ship, or aircraft, supplies areoften stolen or confiscated by governments or persons wishing toestablish regional political or military dominance. Consequently, thecost of delivery is high and the effectiveness of providing real reliefis minimal.

It has been surprisingly discovered that a cost-effective pack ofsupplies can be manufactured and air dropped for distribution to largenumbers of people with a minimized risk of damage to structures on theground, to the supplies themselves, and with minimal risk of harm topeople and animals on the ground, all while maximizing the receipt ofsupplies to those in need. Whereas conventional delivery methodstypically maximize the quantity delivered, such as bulk delivery bytruck, ship, or air, the invention described herein is directed todelivering large numbers of low-weight packs by air so that the packsare distributed evenly and randomly over a large predetermined area.Delivering large numbers packs over a region makes it difficult orimpossible for all supplies to be stolen or otherwise sequestered byindividuals who are not the intended recipients. This effectivelydestroys the black market potential that can be created when suppliesare delivered in bulk, whether that delivery is by truck, ship or air,and, more importantly, maximizes the quantity of supplies received bythe targeted persons.

Preferably, each pack is configured as a single delivery unit and packsare delivered in large numbers, so the risk of supplies not reaching theintended victims or being otherwise stolen is minimized. As aspect onthe invention is therefore the rapid construction and assembly of packsin large numbers. Single station, and semi automated manufacturingapparatus are configured to produce thousands to tens of thousands ofpacks per day. Packs preferably contain one or only a few rations of thesupplies such as, for example, food, water, or medicine. Although thesupply lasts for a short time, because costs are minimized, deliveriescan be repeated many times and with minimal risk to those involved.Importantly, because packs are delivered by air, relief workers neverneed to enter the disaster area itself. Also, depending on theaerodynamic components of the pack, distribution can be from almost anyaltitude, again keeping relief workers safe from danger.

Packs are capable of being distributed or broadcast over a wide area ortargeted to a precise or limited location, again so as to minimize therisk of theft and/or to reach a target area that is itself limited orsmall. The range is preferably pre-determined so as to maximizedistribution to individuals in need as compared to palette distributionby truck, air, or ship.

Packs are configured to possess an aerodynamic component to reduce oreliminate acceleration produced by gravity. Because pack weights aresmall as compared to bulk supplies, the aerodynamic component iscorrespondingly minimized. Preferably the packs themselves areaerodynamically designed so that the rate at which the packs fall to theground is minimized as compared to freefall. Preferably the packs hitthe ground at speeds that pose little to no risk of damage tostructures, other things on the ground, or the contents of the packsthemselves, and little to no risk of harm from to persons or animals(i.e. from the pack landing on a person or animal during descent). Therate and speed are precisely controlled by the aerodynamic component ofthe pack itself by introducing one or more drag and/or lift elements.Drag can be induced from lift or parasitic as a consequence of thestructure of the component. Aerodynamic components that can be addedinclude, but are not limited to one or more wings, fins, tailstructures, propellers or rotary blades, airfoils, sails or parasails,streamers, tunnels, dimples, vent slits, scalloped edges, serrated edgesand parachutes. Preferably, wings or airfoils are configured to forcethe pack to circle or oscillate while descending so as to localize packdelivery to a limited area. While weather conditions can still beproblematic, when known or predicted in advance, specific aerodynamiccomponents can be configured by one skilled in the art to adjust thetrajectory of the packs and therefore account for expected transversemovement of the pack through the air while descending. Also, packdistribution can be monitored by radar (e.g. doppler) or trackingdevices within each pack (e.g. GPS) to plot broadcast distributionpatterns over various terrain and in various weather conditions. Thosepatterns can be used to determine optimal distribution or determine ifre-distribution is necessary. Design configurations may include, forexample, ailerons and rudder structures that may be fixed topredetermined positions, wings and/or leading edges set at apredetermined shape or angle of attack, asymmetric loading of thesupplies in the pack itself and/or combinations thereof.

Alternatively, packs and also boxes containing multiple packs may berendered transparent or invisible to radar by coating pack and/or boxwalls with radar absorbing materials such as, for example, carbon fiberand/or carbon nanotubes including single-walled, double-walled and/ormulti-walled carbon nanotubes. Walls may also be angled to provide packsand/or boxes with a low radar profile. Packs and/or boxes may also becamouflaged with color to render packs invisible from the ground or atleast difficult to spot and track in the air as they descend. Preferredcolors include traditional camouflage patterns, or solid colors orpatterns of sky blue, snow white, gray, brown, green, sand colored, darkblue, and black. Packs and/or boxes may also be colored differentiallyso that the chosen color renders the pack largely invisible when lookingup and difficult to see when on the ground such as, for example, byusing boxes with sky blue bottom and black tops.

Preferably, packs, including the aerodynamic components, aremanufactures as single units to minimize manufacturing costs. Alsopreferable, supply items are inserted into the packs during themanufacturing process, again to minimize costs.

As embodied and broadly described, the disclosures herein providedetailed embodiments of the invention. However, the disclosedembodiments are merely exemplary of the invention that is embodied invarious and alternative forms. Therefore, there is no intent thatspecific structural and functional details should be limiting, butrather, the intention is that they serve as a representative basis forteaching one skilled in the art to variously employ the presentinvention.

FIGS. 1-10 illustrate a pack 10 with an item 11 for aerial delivery. Thepack 10 includes an inner package 12 and an outer package 14. The innerpackage 12 may be disposed along a substantially central longitudinallyextending axis of the outer package 14, for example. The inner package12 either is the item 11 for aerial delivery, or houses the item 11 foraerial delivery. For example, the item 11 may be a mosquito net or waterdisposed in the inner package 12. In the embodiment shown, each of theinner package 12 and the outer package 14 of the pack 10 has aquadrilateral shape in plan view. It should be appreciated that theinner package 12 and the other package 14 may have other shapes in planview, such as a circle, an oval, a triangle, an asymmetrical shape, andthe like, as desired Likewise, an overall size of the pack 10 willdepend on a number of factors, including the size and weight of contentsof the inner package 12, including the item 11 for delivery. In apreferred embodiment, the dimensions of the outer package are 300 mm by150 mm, 350 mm by 200 mm, 400 mm by 300 mm, 450 mm by 200 mm, or anothersize. The ratio of size to weight can be adjusted as required to changethe aerodynamic features of the pack 10.

The outer package 14 may be formed from a polymeric material, such aspolyethylene, for example. In certain embodiments, the outer package 14is formed from a biodegradable material, such as, for example, apolyvinyl alcohol (PVA), polyethylene (PE), polypropylene (PP), orpolystyrene (PS). Plastic boxes have the advantage of allowing forextrusion manufacturing and sealing of the boxes with heat to fuse theplastic materials providing a barrier to moisture and other substances,e.g., rendered water-tight. In preferred embodiments, the outer package14 may also be formed from a mesh material. In preferred embodiments,the outer package 14 is formed from a high performance barrier plastic.For example, the high performance barrier plastic can be an oxygen orcarbon dioxide scavenger or barrier. Additionally, outer package 14 maybe made of numerous layers and/or corrugated to provide strength. Forexample, outer package 14 may have inner and outer layers ofpolyethylene and a middle layer of rip-stop nylon. In preferredembodiments, outer package 14 may be coated with a low friction coating(e.g. a lubricant, talcum powder, Teflon, an oil, or graphite).Furthermore, there may be adhesive between the layers, layers thatpromote heat seals, and layers that provide optical clarity oropaqueness. Furthermore, the thickness of outer package 14 can varydepending on the desired attributes of the pack 10. A skilled artisanmay select suitable materials and number of layers for the outer package14, as desired.

The inner package 12 is disposed inside the outer package 14. Where theinner package 12 houses item 11, the contents of the inner package 12may dictate the particular material used to form the inner package 12.For example, the material forming the inner package 12 may be dictatedby a desired shelf-life and storage time of the item 11 housed by theinner package 12. In preferred embodiments, the inner package 12 isformed from a polymeric material, such as, for example, PE, PVA, PSand/or PP. The inner package 12 may alternatively be formed from anyconventional material known in the packaging industry, materials such asa cardboard, a metal, a plastic, a fabric or a combination of theforegoing, as examples. Furthermore, inner package 12 may be made of orcontain a cushioning material. For example, inner package 12 may beformed from bubble wrap or foam.

As non-limiting examples, the inner package 12 may contain or benon-perishable items 11, such as mosquito netting, a blanket, tools,illuminating devices, batteries, tents or other shelter, rain suits orother clothing and foot protection, toilet tissue, cleansing wipes,ammunition, dental hygiene supplies, parts required for vehicle orequipment repair, hunting and fishing tools, water purification pills, afiltered drinking straw to remove contaminants from water, communicationand/or navigation devices, heating devices such as those chemicallyactivated to generate heat, and video or paper informationalinstructions furnished to victims of a natural disaster or war. Othertypes of non-perishable items 11 may also be housed by the inner package12, within the scope of the present disclosure.

Where the contents of the inner package 12 are non-perishable, the innerpackage 12 may particularly be formed from a biodegradable material,such as a polyvinyl alcohol (PVA), for example, or from a perforatedmaterial. Furthermore, the inner package 12 may include one or more tabscoupled to each end of the item 11 contained therein and to the outerpackage 14. The tabs facilitate a removal of the inner package 12 fromthe outer package 14, for example.

The inner package 12 may also be used for delivery of perishable items11. For example, the inner package 12 may contain a food or a liquidthat requires a substantially fluid and/or light and/or air impermeablematerial. Where the contents of the inner package 12 are temperature orlight sensitive, such as a medication, or flammable, such asfire-starting kits, magnesium blocks for starting fires, or fuels, theinner package 12 may be formed from a thermally insulating material, forexample, a metallic or composite foil. The inner package 12 may alsoinclude a heating or cooling substance or a device to maintain thecontents of the inner package 12 at a desired temperature. The heatingor cooling substance or device may also be contained by the outerpackage 14 and not merely the inner package 12. Medicinal contents ofthe inner package 12 may include insulin, tetanus vaccinations,Dengue-fever vaccinations, malaria vaccinations, antibiotics, and thelike, as non-limiting examples. Other types of perishable items 11 mayalso be housed by the inner package 12, as desired.

The outer package 14 and the inner package 12 may be formed from thesame material or from different materials, as desired. A skilled artisanmay select suitable materials for the inner package 12 and the outerpackage 14, as desired.

With renewed references to FIGS. 1-10, the outer package 14 is formedfrom a pair of superposed sheets 16, 18, having facing surfaces that arejoined together. The top edges of the sheets 16, 18 are sealed togetherto form a top edge seal 20 of the pack 10. Likewise, the bottom edges ofthe sheets 16, 18 are sealed together to form a bottom edge seal 22 ofthe pack 10. The side edges of the sheet 16 are sealed to correspondingside edges of the sheet 18 to form a pair of opposing side edge seals24, 26 of the pack 10. The facing surface of the sheets 16, 18 adjacentthe inner package 12 are sealed together to form mid-pack seals 28, 30of the pack 10. The top edge seal 20, the bottom edge seal 22, and themid-pack seals 28, 30 confine the inner package 12 within the outerpackage 14, for example, as shown in FIG. 6.

The outer package 14 includes at least one aerodynamic component 32, 34.Aerodynamic component 32, 34 preferably creates drag during the freefall of pack 10 during use thereby slowing the descent of pack 10.Additionally, aerodynamic component 32, 34 may provide aerodynamic andstability characteristics such as lift, directional control, thrust, orweight. In the embodiment shown in FIG. 1-10, the at least oneaerodynamic component 32, 34 includes a pair of flanges or wings 32, 34formed between the side edge seals 24, 26 and the mid-pack seals 28, 30of the pack 10. The wings 32, 34 are formed by folding correspondingside edges of the sheets 16, 18 and sealing the folded edges to formwing seals 36, 38, for example, as shown in FIGS. 5 and 7. As a resultof sealing the folded edges to form the wing seals 36, 38, the wings 32,34 normally are closed and extend inwardly along a longitudinal axis ofthe pack 10. The wings 32, 34, which as shown in FIGS. 1-2 are normallyclosed in the pack 10, unfurl as shown in FIGS. 3-4 as the pack 10 isdropped through the air. While two wings 32, 34 are depicted, any numberof wings can be used. Figure depicts the stages of forming wings 32, 34.Pack 10 is feed into the wing forming mechanism at infeed 205, the firstportion of the wings are formed at forming area 210, the second portionof the wings are formed at forming area 215, the third portion of thewings are formed at forming area 220, the forth portion of the wings areformed at forming area 225, the fifth portion of the wings are formed atforming area 230, the edges of the wings are sealed at edge sealing 235,the pack 10 enters reflex area 240 where the wings are flexed open 245,and finally the pack 10 is sent to the packout area 250. The individualpacks are separated from the joined packages being produced via aguillotine type cutting device and then subsequently sent to packoutareas.

The at least one aerodynamic component 32, 34 may advantageously causeturbulent flow, as opposed to laminar flow, across the outer package 14and decrease a descent rate of the pack 10 in operation. Preferably, thevelocity of pack 10 is reduced from freefall to, for example, 20 metersper second, 15 meters per second, 10 meters per second, 8 meters persecond, or 5 meters per second. Preferably, the impact with the groundof pack 10 is reduced from the impact of the pack with ground duringfreefall, for example, by 90%, 75%, 60%, 50% or another percentage.Although the embodiments shown in FIGS. 1-10 include wings 32, 34 as theat least one aerodynamic component 32, 34, one of ordinary skill in theart should understand that the at least one aerodynamic component 32, 34may alternatively include a tail, a fin, an airfoil, a parasail, aparachute, rotary blades, streamers or a tail (see FIG. 18), or otherstructure adapted to create drag when the pack 10 is dropped through theair. As a non-limiting example of other types of structure, tunnels,dimples, vent slits (see FIG. 19), scalloped or serrated edges (see FIG.20), or holes formed in the outer package 14 may be used to for createturbulent flow. Suitable aerodynamic component 32, 34 for the pack 10may be selected, as desired. Furthermore, a combination of aerodynamicelements can be used. For example, as shown in FIG. 21, holes can bepunched into wings 32, 34 to further control drop rate and/or flightcharacterizes.

FIGS. 26, 27 and 28 show additional embodiments of a pack 10. Theembodiments shown in FIGS. 26, 27 and 28 include air vents 2610, 2710,and 2810. Preferably, air vents 2610, 2710, and 2810 allow a portion ofair the air passing over pack 10 to, instead, pass though pack 10 aspack 10 descends. Such airflow increases the ability of the packs toseparate from each other during deployment and changes the aerodynamicsof the packs. Air vents 2610, 2710, and 2810 can be positioned at theends of pack 10, on the sides of pack 10, in the middle of pack 10, orat another location. Furthermore, there can be multiple air vents 2610,2710, and 2810 and a combination of air vents 2610, 2710, and 2810through pack 10. Each of the apertures for air vents 2610, 2710, and2810 penetrates at least one portion of the upper surface of pack 10 andone portion of the lower surface of pack 10. The apertures in the upperand lower surfaces of pack 10 can be in-line or apart from each other,thereby allowing air into pack 10 through one aperture and allowing airto exit pack 10 through another aperture.

Air vent 2610 is preferably comprised of a mesh screen or another airpermeable material. While air vent 2610 is shown as square in shape, airvent 2610 can have another shape (e.g. rectangular, ovular, circular, ortriangular). Air vent 2710 is preferably a cutout from the body of pack10. While air vent 2710 is shown as ovular in shape, air vent 2610 canhave another shape (e.g. rectangular, square, circular, or triangular).Air vent 2810 is preferably a cutout from the body of pack 10 with flaps2815 coupled to the perimeter of air vent 2810. Preferably, flaps 2815are of the same material as the body of pack 10, however flaps 2815 canbe of another material. In a preferred embodiment, flaps 2815 arecreated by cutting an “X” into the body of pack 10, however flaps 2815can be attached to pack 10 (e.g. with adhesive or fused to pack 10).While air vent 2810 is shown as square in shape, air vent 2810 can haveanother shape (e.g. rectangular, ovular, circular, or triangular).

In certain embodiments, the aerodynamic component 32, 34 control theflight path of the pack 10. For example, wings may be formed to forcethe pack 10 to follow a spiral descent, a zigzag descent, or a descentsimilar to an airplane that is landing. Such controlled descent improvesthe accuracy of delivering packs 10 to a desired location.

In certain embodiments, the outer package 14 is formed from asubstantially rigid material adapted to militate against a folding ofthe pack 10. With reference to FIGS. 5 and 8, the outer package 14 mayalso include at least one rigid insert 40, 42 adapted to providestructural support to the outer package 14 and militate against anundesirable folding of the pack 10 in operation. For example, the rigidinserts 40, 42 may be elongate members sealed and disposed between themid-pack seals 28, 30 and the wing seals 36, 38 of the outer package 14.The rigid inserts 40, 42 may include ribs laterally oriented within theouter package 14, or supports longitudinally oriented within the outerpackage, for example. The rigid inserts 40, 42 may also be coupled tothe outer package 14 during the formation of the top edge seal 20 andthe bottom edge seal 22. It is understood that the inserts 40, 42 may becoupled to the top edge seal 20 and the bottom edge seal 22, as desired.The inserts 40, 42 may also be disposed adjacent the inner package 12 orcoupled to an exterior of the outer package 14. In a preferredembodiment, the rigid inserts 40, 42 may include stiff or folded paperinformational instructions for users of the contents of the pack 10 (seeFIG. 22). In other embodiments, the rigid inserts 40, 42 are cardboardor plastic inserts having a stiffness sufficient to militate against afolding of the outer package 14. One of ordinary skill in the art mayselect a suitably rigid material for the inserts 40, 42, as desired withmaintaining the desired flexibility. Outer package 14 can also haveembossed surfaces, vacuum sealed portions, pressurized chambers and/orchambers filled with gas (e.g. helium, hydrogen, or air) to adjust thestiffness of the pack 10.

As established hereinabove, the inner package 12 either is the item 11for aerial delivery, or houses the item 11 for aerial delivery. As shownin FIG. 9, where the inner package 12 houses the item 11 for delivery,for example, water, the inner package 12 may be coupled with the outerpackage 14. In particular, a top edge 44 and a bottom edge 46 of theinner package 12 may be sealed between the sheets 16, 18 with a toptransverse seal 48 and a bottom transverse seal 50, respectively. Asshown in FIG. 10, where the inner package 12 is the item 11 for aerialdelivery, the inner package may be loosely disposed between the sheets16, 18 of the outer package 14. A plurality of the items 11individually, or packaged within a plurality of the inner packages 12,may also be substantially evenly distributed within the outer package 14of the pack 10. It should also be appreciated that the inner packages 12may also be substantially evenly distributed along a length of the outerpackage 14 in order to provide a balanced weight distribution andfacilitate the delivery of the pack 10 through the air (see FIG. 23).Other means for disposing the inner package 12 within the outer package14 of the pack 10, and any number of items 11, may be used as desired.Furthermore, more than one inner package 12 may be disposed throughoutouter package 14. Preferably, the inner packages are disposed evenly toevenly distribute the weight throughout outer package 14. In a preferredembodiment, item 11 is allowed to move freely within inner package 12.In a preferred embodiment, pack 10 holds 100 grams, 200 grams, 300grams, 400 grams, 750 grams, 1 kilogram, 2 kilograms or another amountof item 11. The size, flexibility, aerodynamic element(s), material, andpositioning of item 11 can all be adjusted depending on the weight andcontents of item 11. Furthermore, item 11 can be position so that pack10 has a positive static stability, a neutral static stability, or anegative static stability.

Preferably, the content of pack 10 is a single serving or ration of item11. For example, the contents can be a single serving of water, a singlenutrition bar, a first aid kit, or a sanitation kit. In embodimentswhere pack 10 holds a single serving of item 11, distribution of thepacks is achieved during the airdrop since the packs will preferably beevenly and randomly distributed across the drop zone.

It is understood that the various seals 20, 22, 24, 26, 28, 30, 36, 38,48, 50 of the present disclosure may be formed by a chemical sealingoperation, such as by use of an adhesive or a chemical solvent, forexample, or by a heat welding operation, as desired. In particularlyillustrative embodiments, the various seals 20, 22, 24, 26, 28, 30, 36,38, 48, 50 are formed by heat sealing operations. Alternative means forforming the various seals 20, 22, 24, 26, 28, 30, 36, 38, 48, 50 mayalso be employed, as desired.

The pack 10 of the present disclosure may further include a perforation52 to facilitate an opening of the pack 10. The perforation 52 may be atamper-proof or tamper-evident perforation 52. The perforation 52 mayextend inwardly from an edge of the emergency pack and traverse at leastone of the top edge seal 20, the bottom edge seal 22, the top transverseseal 48, and the bottom transverse seal 50, in order that the same sealsmay be opened to permit access to the inner package 12 and the item 11for aerial delivery by an end user of the pack 10. Additional, as shownin FIG. 24, perforations may be added to form a pouch with a carryinghandle.

As established herein, the outer package 14 is adapted to contain theinner package 12. The outer package 14 may also contain an illuminatingdevice to facilitate visible location of the pack 10, particularly atnight, such as a flashing LED, glowing film, or a reflective device, forexample. The illumination device may be activated by time, temperature,pressure, or impact, for example. Alternatively, the outer package 14may be formed from a radar reflective material or a radar dissipatingcoating. In certain embodiments, the outer package 14 is formed from orcoated with a light-activated substance. The outer package 14 may alsocontain a tracking device such as a GPS device, an RFID device, and thelike to facilitate tracking of the pack 10 or for inventory control.Furthermore, the packaging may contain a noise generating device. Forexample the packaging may contain a whistle, buzzer, or beeper that isactivated as the air passes over the packaging, electrically, ormechanically. The noise generating device can announce the arrival andlocation of the packs as they drop or at the drop location. In certainembodiments, pack 10 has no moving parts, electric parts, or mechanicalparts.

The outer package 14 may include and/or contain indicia. The indicia mayinclude a colored material or a symbol to indicate the contents thereof.For example, blue indicium may indicate that the item 11 is water, a RedCross indicium may indicate that the item 11 includes medical supplies,and the like. The indicia may also include instructions in a pluralityof languages or graphical instructions for opening the pack 10 and toindicate the use of the contents thereof. In certain embodiments, thepacks 10 may be colored. For example, the packs 10 may be blue, maroon,yellow, beige, or patterns such as plaid or polka-dotted. Additionally,the pack 10 may have a solar film with a printed circuit device coupledto the pack. The device can be used for communication and/or navigationproposes by receiving and sending AM/FM or shortwave signals.

To aerially distribute the packs 10, a skilled artisan may select anysuitable aerial distribution system, as desired. As non-limitingexamples, the distribution system may be substantially as described inU.S. Pat. No. 4,349,168 entitled “Cargo Delivery System for Aircraft,”hereby incorporated herein by reference in its entirety; U.S. Pat. No.4,241,890 entitled “Aerial Delivery System,” hereby incorporated hereinby reference in its entirety, and U.S. Pat. No. 4,374,578 entitled“Aerial Cargo Delivery System,” hereby incorporated herein by referencein its entirety.

FIGS. 29a and 29b depict an embodiment of an aerial storage anddistribution container 2900. Container 2900 is preferably made ofcardboard. However container 2900 can be made of other materials, forexample, plastic, metal, nylon, wood, cloth, rubber, Styrofoam, or othernaturally occurring or manmade materials. While container 2900 is shownas a cube, container 2900 can have other shapes. For example container2900 can be a cylinder, a pyramid, a cuboid, a cone, bag (for example asdepicted in FIGS. 35a-c ), bladder bag (e.g. for attachment to thebottom of a helicopter), or a prism. In the preferred embodiment,multiple containers 2900 can be stacked one on top of another. Eachcontainer 2900 is preferably able to hold up to 5,000 packs 10, howevereach container 2900 can hold more or less packs 10.

In the preferred embodiment, the upper surface of container 2900 issealed with an adhesive tape that includes a pull cord 2905. Pull cord2905 is preferably embedded in the adhesive tape and when pulled, priorto deployment of the contents of container 2900, pull cord 2905 dividesthe adhesive tape along a seam in the upper surface of container 2900.In other embodiments, container 2900 can be temporarily sealed withglue, bolts, brads, rivets, screws, nails, interlocking lids, frictionlids, screw top lids, other adhesives, locks, twine, rope, or otherfastening devices.

Preferably, there is a tether 2910 coupled to the bottom surface ofcontainer 2900 (as shown in FIG. 29b ). Tether 2910 can be coupled tothe bottom surface of container 2900 by adhesive, bolts, rivets, brads,screws, nails or another fastening device.

Furthermore, tether 2910 can be incorporated into the material of thebottom surface of container 2900 or can be coupled to the inside ofcontainer 2900 through a hole in the bottom surface of container 2900.Tether 2910 may be temporarily affixed to a side of container 2900 (asshown in FIGS. 29a and 29b ) with adhesive, bolts, rivets, brads,screws, nails, twine, rope or another fastening device. Tether 2910 ispreferably made of a flexible, high strength, inelastic material, suchas nylon, rubber, chain, plastic, or other naturally occurring ormanmade materials. In the preferred embodiment, tether 2910 has a loop2915 at the end of tether 2910 opposite the end that is coupled tocontainer 2900. Loop 2915 may be couplable to a static line in anaircraft or another portion of an aircraft. In the preferred embodiment,tether 2910 is affixed to a surface of container 2900 that is parallelto pull cord 2905 (as shown in FIGS. 29a and 29b ). However, tether 2910can affixed to a surface of container 2900 that is perpendicular to pullcord 2905. Container 2900 may have handholds. The handholds can extendfrom the body of container 2900 or may be cut into the surface ofcontainer 2900. The bottom surface of container 2900 may additionallyhave a slider coupled thereto. The slider assists in forcing container2900 out of the vehicle and distributing the contents. For example, theslider can be a low friction disk, a semispherical plastic device,rollers, casters, wheels, or another device.

Container 2900 can be reusable or recyclable or repurposed.Additionally, in embodiments where container 2900 is released from thevehicle at the location of deployment, container 2900 may berepurposable for a secondary use. For example, container 2900 may becoated with a waterproof coating so container 2900 can be used as ashelter, container 2900 may be impregnated with a material (e.g. wax) toincrease the burning time of container 2900, or container 2900 can beinsulated to keep in or out heat.

To deploy the contents of container 2900, in the preferred embodiment,container 2900 is loaded onto a vehicle (e.g. a cargo plane). Dependingon the amount of contents that needs to be deployed, one or morecontainers 2900 can be loaded onto the vehicle. Once loaded, loop 2915of tether 2910 is coupled to a static line of the vehicle. Preferably,container 2900 is positioned within the vehicle so that tether 2910 isfacing the inside of the vehicle and the opposite side of container 2900is facing the opening through which the contents will be deployed. Oncecoupled to the static line, pull cord 2905 is pulled, thereby unsealingcontainer 2900. When the vehicle arrives at the location of deployment,container 2900 is forced out of the vehicle and releases the contents.

Container 2900 may have one or more dispersal aids installed tofacilitate the packs 10 exiting container 2900 without clumping orotherwise remaining together. For example, as shown in FIGS. 35a -b,container 2900 may be equipped with a deflector 3590. Deflector 3590 ispreferably foam, however other materials can be used (e.g. cardboard,plastic, wood, metal, or other naturally occurring or manmadematerials). As the packs 10 exit container 2900, deflector 3590interferes the exit of the outer rows of packs 10 causing the packs 10to disperse.

FIGS. 36a-b depict an embodiment of another dispersal aid 3692.Dispersal aid 3692 is preferably a ridged board coupled to a foampyramid 3694. Pyramid 3694 can alternatively be cardboard, plastic,wood, metal, or other naturally occurring or manmade materials.Dispersal aid 3692 is preferably coupled to an opening in container 2900and as tether 2910, which is coupled to pyramid 3694, is pulled,dispersal aid 3692 is forced through container 2900 thereby dispersingpacks 10. The opening in container 2900 may be secured by adhesive,elastic banding or another fastening device.

Another embodiment of a dispersal aid is shown in FIG. 37. In theembodiment of FIG. 37, packs 10 are placed between interweaves of a thinsheet of film 3796. Film 3796 can be plastic, paper, cloth, or anothernaturally occurring or manmade material. As container 2900 is deployed,film 3796, along with packs 10 placed between the folds of film 3796,exits container 2900. Due to the folds in film 3796, packs 10 are forcedfrom container 2900 in multiple directions.

FIG. 38 depicts an embodiment of another dispersal aid. In theembodiment of FIG. 38, a divider 3893 is placed within container 2900.In the example shown, divider creates four sections within container2900, however another number of sections can be created by divider 3898.Preferably, divider 3898 is of the same material as container 2900,however another material can be used. Divider 3898 allows packs 10 to bestacked without overlapping. However, in other embodiments, packs 10 canbe randomly placed within each section or interleaved. In a preferredembodiment, a deflection device can be installed at the centralintersection between the portions of divider 3898 to further dispersepacks 10.

FIGS. 50A-F depict an embodiment of another dispersal aid. In theexploded view depicted in FIG. 50A, as the box 5000 is deployed, airpulls lid 5050 off box 5000 and pulls an inner bag 5055 out of box 5000.For example, lid 5050 can be coupled to inner bag or flexible liner 5055at attachment point 5054 via paracords or tethers 5053. Preferably, asshown in FIG. 50C, attachment point 5054 is a reinforcement material andgrommet 5052 couples tethers 5052 to inner bag 5055. Preferably, tethers5053 are coupled to lid 5050 via grommets 5056 and nuts 5057 in lid5050. Other methods of coupling tethers 5052 to both lid 5050 and innerbag 5055 can be implemented.

Preferably, inner bag 5055 is forced inside out and packs 10 withininner bag 5055 are forced out of box 5000. As inner bag 5055 inverts,preferably a breakaway bottom 5058 is pulled through box 5000 to assistin forcing packs 10 out of box 5000. Preferably, an edge of inner bag5055 is folded over the edge of box 5000 and the edges of inner bag 5055and box 5000 are sewn together. In certain embodiments, a parachute orother device may be coupled to lid 5050 to further assist in ejectingpacks 10 from box 5000.

FIG. 50B depicts a view of box 5000, lid 5050, and inner bag 5055 afterdeployment with inner bag 5055 inverted and having ejected its contents.FIGS. 50D-F depict various views of lid 5050, inner bag 5055, and bottom5058.

FIGS. 30a-c depict another embodiment of an aerial storage anddistribution container 3000. Container 3000 is similar to container2900, however container 3000 further comprises a canopy 3037. The canopy3037 is preferably an air resistant device. For example, canopy 3037 canbe a parachute, a parasail, a wing, or a rotatable copter. The canopy3037 is preferably composed of a durable, light weight material. Forexample canopy 3037 can be made of nylon, cotton, canvas, silk, mylar,rubber, or another naturally occurring or man-made material.Additionally, the canopy 3037 may be repurposable for a secondary use.For example, canopy 3037 may be water proof to use as a shelter, canopy3037 may have handles to convert to a bag, or canopy 3037 may bereflective to use as a solar powered stove.

The canopy 3037 can be stored within or without container 3000 or can beloose. For example, in the embodiment shown in FIGS. 30a and 30b ,canopy 3037 can be stored in a receptacle 3030 coupled to the inside lidflap 3035 of container 3000. Preferably, canopy 3037 is coupled totether 3010. During deployment of the contents of container 3000, astether 3010 is pulled, canopy 3037 is preferably released and unfurls inthe air due solely to wind resistance. In the embodiment shown in FIGS.30a and 30b , for example, canopy 3037 is pulled through opening 3040 incontainer 3000. Container 3000 is then released from the transportationvehicle and canopy 3037, still attached to tether 3010, forces container3000 to rotate so that the opening is facing toward the earth and, thus,to empty. Additionally, canopy 3037 preferably slows the decent ofcontainer 3000 to prevent injury or damage to people or objects on theground. The canopy 3037 and/or container 3000 can be outfitted with anindication device. The indication device can alert people on the groundof the falling container and can direct people to the container 3000once on the ground. The indication device, for example, can be a light,smoke, a noise maker (e.g. whistle), a GPS indicator, or a reflectivesurface.

FIGS. 49a-b depict another embodiment of a canopy. In the embodimentdepicted in FIGS. 49a -b, the box lid 4950 acts as a canopy, slowing thedescent of box 4900 during deployment. Preferably, box lid 4950 isattached to box 4900 via tethers 4910 at grommets 4911. Preferably, asbox 4950 is deployed, box lid 4950 lifts off box 4900 and pulls tethers4910 taught. As tethers 4910 tighten, preferably straps 4915 pulls afalse bottom 4956 out of box 4900, thereby forcing the contents of thebox out through the bottom of the box.

FIGS. 31a-d depict another embodiment of an aerial storage anddistribution container 3100. Container 3100 is similar to container2900, except the bottom of container 3100 has a staggered slot 3150.Staggered slot 3150 preferably forces tether 3110 to weave throughseveral layers of the bottom of container 3100. As shown in FIG. 31a ,tether 3110 weaves through staggered slot 3150, making three turns.While three turns are shown, another number of turns can be implemented.Preferably, tether 3110 is coupled to a board 3155 that fits within thebottom of container 3100. Board 3155 can be masonite, plywood, metal,plastic, cardboard, or another material. Tether 3110 can be coupled toboard 3155 by friction, a slip knot, rivets, bolts, brads, adhesive,screws, or another fastening device.

Staggered slot 3150 aids in sealing the bottom of container 3100 andpreferably reduces the forces experienced by container 3100 as it isdeployed. Preferably, during deployment of container 3100, the materialof container 3100 rips as tether 3110 straightens, thereby slowing thetautening of tether 3110 and reducing the pressure on board 3155.

As shown in FIG. 31b -d, tether 3110 preferably exits the bottom ofcontainer 3100, and is secured to one side and the top of container3100. Preferably, tether 3110 is secured to container 3100 by papertape, however other fastening devices can be used (e.g. adhesive, bolts,rivets, brads, screws, nails, twine, rope or another fastening device.Preferably, tether 3100 covers and seals the seam between the twoportions of the lid of container 3100. As container 3100 is deployed,preferably, the seam between the two portion of the lid of container3100 becomes unsealed, thereby allowing the contents of container 3100to exit container 3100.

FIGS. 32a-b depict another embodiment of a container 3200. The top ofcontainer 3200 preferably unfold to form a chute 3260 through which thecontents of container 3200 can be dispersed from a vehicle. Container3200 may be able to be coupled to a tipping pallet 3265 to assist indirecting the contents of container 3200 out of the vehicle.

FIGS. 43a-f depict another embodiment of a container 4300. In theembodiment of FIGS. 43a-f , the container is preferably comprised of asingle piece of corrugated plastic, cut and folded into a closable box.Preferably both the top and bottom of container 4300 are sealablewithout the use of a sealing device (e.g. tape, fasteners, or twine). Inthe preferred embodiment, container 4300 has at least one tab extendingfrom the top of the box and at least one indentation or hole in thebottom of the box to allow multiple boxes to be stacked on top of eachother. Preferably, the seams of container 4300 are heat sealed.

FIGS. 39a-c depict an embodiment of a container bag 3900. Bag 3900preferably is collapsible for shipping as depicted in FIG. 39a . At theopening of bag 3900, preferably there is a main ring 3944. Main ring3944 preferably has an angled flange on the inner diameter (as shown inFIG. 39c ). The angled flange preferably disrupts flight path of thecontents of bag 3900 during deployment, causing the contents to scatter.Main ring 3944 is held onto bag 3900 by bag retainer ring segments 3946.While two bag retainer ring segments are shown another number can beused (e.g. one ring, three ring segments, or four ring segments).Preferably, the open edge of bag 3900 is held between main ring 3944 andbag retainer ring segments 3946. In the preferred embodiment packdisrupter disk 3948 is coupled to main ring 3944 by straps 3942.

While four straps 3942 are shown another of straps 3942 can couple packdisrputer disk 3948 to main ring 3944. Preferably, during transit, packdisrupter disk 3948 acts as a lid for bag 3900. However, once deployed,pack disrupter disk 3948 is held at a distance from main ring 3944 bystraps 3942. Pack disrupter disk 3948 further disrupts flight path ofthe contents of bag 3900 during deployment, causing the contents tofurther scatter.

In some embodiments, other containers or magazines holding a desirednumber of the packs 10 are disposed in a cargo hold of an airplane, suchas a C-130, for example. Any suitable method for loading the packs 10onto the airplane may be employed. For example, the containers may beloaded on the airplane using the system and method described in U.S.Pat. App. Pub. No. 2008/0219830 entitled “Channel Slide Cargo HandlingSystem and Method,” hereby incorporated herein by reference in itsentirety. The containers may be disposed in rows and columns as iscustomary for the cargo of airplanes. The containers may include desiredquantities of packs 10 and types of supplies, and may be prepared andstored at strategic locations across the U.S. and the world awaitingdistribution in the event of a military operation or natural disaster.

In a preferred embodiment, the containers are placed into a larger bulk(or gaylord) box for storage, shipment, and deployment. The bulk box canbe made of wood, cardboard, plastic, corrugated plastic, metal, oranother ridged or flexable material FIGS. 40a-c depict one embodiment ofa gaylord box 4000. Preferably, box 4000 houses eight containers asdescribed herein, however box 4000 can house another number ofcontainers (e.g. 4, 6, or 10). In the preferred embodiment, box 4000 isreinforced with frame 4010. Frame 4010 can be made of wood, cardboard,plastic, metal, or another ridged material. Preferably, frame 4010 iscoupled to box 4000 via tethers 4020. In the preferred embodiment,tethers 4020 are tied or otherwise attached to frame 4010 and passthrough an opening in the bottom of box 4000. Tethers 4020 can then becoupled to the deployment vehicle (e.g. airplane) or to a canopy. Duringdeployment, box 4000 is jettisoned from the deployment vehicle and isforced upside down, either by the canopy or by the tethers beingattached to the deployment vehicle. Once upside down, the smallercontainers exit box 4000 and empty their contents by one of the methodsdescribed herein.

FIG. 41 depicts another embodiment of a gaylord box 4100. Box 4100 issimilar to box 4000, however instead of a frame, the bottom surface ofbox 4100 is defined by a pallet 4130. Pallet 4130 can be made ofcardboard, wood, plastic, metal, or another ridged material. Preferably,both box 4100, which fits over pallet 4130 or is sealable to the pallet,and pallet 4130 have openings for a forklift to engage for ease ofloading onto the deployment vehicle. Box 4100 and pallet 4130 can besealed together via folding the material of box 4100 into pallet 4130,welding, rivets, bolts, adhesive, or other fastening devices. FIG. 46depicts an embodiment of a gaylord box coupled to a pallet with portionsof the gaylord box inserted into the bottom surface of the pallet andthen folded over. Preferable, pallet 4130 and box 4100 are both loadedonto the deployment vehicle and are both jettisoned from the deploymentvehicle at the location of deployment. FIG. 45 depicts an exploded viewof an embodiment of a loaded gaylord box coupled to a pallet.

FIGS. 44a-b depict another embodiment of a pallet 4400. In theembodiment shown in FIGS. 44a -b, the pallet is comprised of acorrugated plastic top and bottom and foam supports. Preferably, thefoam supports prevent dipping or sagging of the top while loaded. Thematerial of the pallet 4400 provides durability, is light weight, andelastic compared to traditional wood pallets. Pallet 4400 may besealable to a gaylord box made of corrugated plastic, and once sealed,the pallet and gaylord box may be water tight. Pallet 4400 may beotherwise coupleable to a gaylord box such that the pallet and gaylordbox do not separate during deployment. Preferably, the bottom of pallet4400 is proud of the rest of pallet 4400 providing a flange that canmate with an aircraft container delivery system (CDS). Preferably, theflange allows the pallet to be used as a skid board. To increase thestrength of the skid board, preferably two sheets of superimposedcorrugated plastic are coupled together orthogonally to create thebottom of pallet 4400.

FIGS. 48a-c depict embodiments of a box, container, or gaylord with hookand loop strapping 5 holding the cover or lid 4 of the box to the bodyof the box 3. FIG. 48d is an exploded view of a box 3 with the strapping5 The strapping 5 may be coupled to parachute rigging 1 or a retentionsystem for the box 3. The strapping 5 preferably insures lid 4 andproduct retention during transport and subsequent box 3 and lid 4containment within the parachute rigging during aerial deployment. Whenstoring or transporting filled boxes 3, it is usually desirable to keepthe box 3 covered so as to reduce product contamination within the box3. For air transport, a box 3 can be subjected to many external forcesand the lidded box 3 preferably is able to retain the product within thebox 3 under many conditions. When aerial deployment of the productresiding within the box 3 is required, the lid 4 is preferablycompletely removed from the box 3 to allow the product to freely exitthe box 3. This lid 4 removal is preferably completed without manualassistance and without the lid 4 being allowed to free-fall from theaircraft. Preferably, the strapping 5 and parachute rigging 1 willretain the lid 4 during transport at forces up to 3 g's or greater byrelying upon the shear strength (preferably 10 lb./in²) of the hook andloop fabric. While the embodiment is described using hook and loopfasteners, other fasteners can be utilized, for example snaps, adhesive,buttons, zippers, bolts, rivits, breakaway fastener, and clips. Duringaerial deployment the parachute bridal portion of the rigging 1preferably acts upon the peel strength (preferably 3 lb./in. of width)of the hook and loop fabric. Preferably both the shear force for lid 4retention and the peel force for lid 4 removal can be modified asdesired by merely changing the dimensions of the hook and loop fabriccomponents. The hook and loop fabric is preferably positioned andattached to both the rigging 1 and box 3 in a manner that utilizes theinherent properties (shear strength and peel strength) of the hook andloop fabric. Preferably, strap 5 is coupled to the bottom of box 3around at least one side of box 3, over lid 4 and engages acorresponding hook or loop fabric along another side of box 3. Strap 5may pass through a portion of either box 3 and/or lid 4 to increasestrength and keep the components together during delivery. 1, 2, 3, 4,or more straps can be used.

In testing the strength of hook and loop fabric, the sheer strength wasabout 10 lbs per square inch and the peel strength was about 3 lbs.There was little variation between the differing length and widths offabrics tested. So the 1″×1″ hook and loop had about a 10 psi shearstrength and a 3 pound peel strength, the 2″×1″ hook and loop had abouta 20 psi shear strength and a 3 pound peel strength and the restfollowed suit. Table 1 is a chart showing the various peel and sheerstrengths for the fabrics tested.

TABLE 1 Shear and Peel Strengths for Hook and Loop Fabric Hook Hook LoopLoop Shear Peel Length Width Length Width Strength Strength 1″ 1″ 1″ 1″10 lbs 3 lbs 2″ 1″ 2″ 1″ 20 lbs 3 lbs 3″ 1″ 3″ 1″ 30 lbs 3 lbs 4″ 1″ 4″1″ 40 lbs 3 lbs 1″ 2″ 1″ 2″ 20 lbs 3 lbs 2″ 2″ 2″ 2″ 40 lbs 3 lbs 3″ 2″3″ 2″ 60 lbs 3 lbs 4″ 2″ 4″ 2″ 80 lbs 3 lbs

During deployment, box 4000 or box 4100 is jettisoned from thedeployment vehicle and is forced upside down, either by the canopy or bythe tethers being attached to the deployment vehicle. Once upside down,the smaller containers exit the box and empty their contents by one ofthe methods described herein. For example, as depicted in FIG. 42, thesmaller containers may be tethered to the box 4000 or to the pallet ofbox 4100 and, once the contents of the smaller containers is deployed,the smaller containers and the box 4000 or box 4100 can descend togetherwith the single canopy coupled to the box 4000 or box 4100 slowing thedecent. FIG. 47 depicts another embodiment of the progress of thecontainers after deployment. In the embodiment depicted in FIG. 47, eachsmaller container has its own canopy, which allows the containers todrift apart during deployment.

In an exemplary embodiment, a rear hatch of the airplane is closedduring transport of the containers to a desired location, and a conveyorsystem disposed underneath the containers is retracted. Once theairplane has reached a desired location, the rear hatch of the airplaneis opened and the conveyor system is extended from the cargo hold. Thepacks 10 in the containers are then emptied onto the conveyor system,and the conveyor system causes the packs 10 to exit the airplane fromthe rear hatch for aerial distribution to people on the ground. It isunderstood that the packs 10 of a container may be emptied en masse, orthe packs 10 may be individually metered onto the conveyor system at adesired rate. The packs 10 are conveyed from the containers and out ofthe airplane so that the packs 10 are not bunched or clustered together,and that separation of each pack 10 from the other packs 10 is achieved.In another embodiment, as depicted in FIG. 33, the deployment vehiclecan be outfitted with a hopper 3370. Hopper 3370 is preferably coupledto one side of the vehicle and can be filled with packs 10 fordeployment at the desired location. Once the vehicle reached thelocation of deployment, at least a portion of hopper 3370 can be liftedto allow gravity to force packs 10 from the vehicle. In anotherembodiment a mechanical conveyor forces packs 10 from the vehicle.Hopper 3370 can be metal, plastic, wood, or other naturally occurring ormanmade materials. If the vehicle is an airplane, the weight of thehopper and its contents may have to be balanced.

In another embodiment, as depicted in FIGS. 34a -c, a cart 3480 can beused to deploy the packs 10 from the vehicle. Cart 3480 may be similarto a wheelbarrow with one wheel or may have multiple wheels. In thepreferred embodiment, cart 3480 is loaded with packs 10 and at thelocation of deployment is tipped out of the vehicle so that packs 10exit cart 3480. Cart 3480 may be outfitted with a tarp 3485 or othercovering to prevent packs 10 from blowing back into the vehicle.Furthermore, cart 3480 may have hooks coupled to the bottom surface thatengage a roller mounted to the exit of the vehicle. The hooks and rollermay assist in tipping cart 3480. Cart 3480 and tarp 3485 can be metal,plastic, wood, or other naturally occurring or manmade materials.

It has also been surprisingly discovered that when a plurality of packs10, as shown in FIGS. 1-10, are distributed from an elevated point abovethe ground such as from an airplane, substantially all of the packs 10are oriented with the aerodynamic component 32, 34 between the sheet 18and the ground. Such orientation results in the aerodynamic component32, 34 being caught by the air and extending outwardly to minimize aterminal velocity of the packs 10. The orientation of the aerodynamiccomponent 32, 34 further advantageously results in a random and evendistribution of the packs 10 across the ground above which the packs 10are deployed.

Due to the size of the packs 10, the proportions of the contents of theof the inner package 12 thereof, and the materials from which the packs10 are formed, the packs 10 are adapted to reach a desired peak terminalvelocity that is sufficiently low such that the pack 10 does not harmpeople or property on the ground. As discussed herein, the size, weight,and nature of the contents of the packs 10 will dictate the materialsused to form the inner and outer packages 12, 14 and the size of thepack 10.

The aerodynamic component 32, 34 of the packs 10 advantageously providea wind resistant structure that further minimizes the terminal velocitythereof. The rigid inserts 40 optionally incorporated into the pack 10provide rigidity to militate against the bending or folding of the pack10 during the aerial distribution. By militating against bending orfolding, the surface area of the pack 10 contacted by air is maximized,thereby reducing, and in some instances minimizing, the terminalvelocity of the pack 10.

By distributing the packs 10 individually rather than on pallets, awider distribution of supplies contained therein may optionally beachieved, and hoarding of the supplies is more difficult, therebyensuring more people receive the necessary supplies.

As shown in FIGS. 11-17, the present disclosure also includes acontinuous system 100 for producing a pack 10. Other types of packs 10may also be manufactured with the system 100 of the present disclosure.

Referring to FIG. 11, the system 100 for manufacturing the pack 10includes a product loading unit 102, a longitudinal mid-pack and edgesealing unit 104, a transverse heat sealing unit 106, a perforator unit108, a wing folding unit 110, a wing band sealing unit 112, and a packseparator unit 114. The system 100 also includes a pair oflongitudinally extending conveyors 116, 118 disposed in sequence,hereinafter referred to as the first conveyor 116 and the secondconveyor 118, for continuously transporting the pack 10 and relatedsubcomponents of the pack 10 through the system 100. Each of the firstconveyor 116 and the second conveyor 118 may be in communication with atleast one vacuum plenum 119 configured to secure the pack 10 and therelated subcomponents of the pack 10 to the first conveyor 116 andsecond conveyor 118 as the pack 10 is manufactured.

With reference to FIG. 12, the product loading unit 102 is configured todeposit an inner package including an item for aerial delivery between afirst sheet and a second sheet. The product loading unit 102 may includea first sheet supply roll 120, a second sheet supply roll 122, and aproduct loader 124. The first sheet supply roll 120 provides the firstsheet, the second sheet supply roll 122 provides the second sheet, andthe product loader 124 provides the inner package for the pack 10. Thefirst sheet supply roll 120 continuously provides the material formingthe first sheet for the pack 10. As the first sheet is advanced from thefirst sheet supply roll 120, a printer may print desired indiciathereon. For example, the printer may be used to print a date ofcreation, date of expiration, tracking information and indicia, and thelike. The first sheet may be advanced through the system 100 by thefirst conveyor 116. One of ordinary skill should understand that thefirst sheet may be advanced through the system 100 by alternative means,such as pairs of cooperating driven rollers, as desired. Additionally,the first sheet may be comprised of multiple layers as described herein.

As the first sheet is advanced adjacent the product loader 124, theinner packages are deposited on the first sheet by the product loader124 at desired intervals. Positive results have been obtained from packs10 having the inner packages disposed along a substantially centrallongitudinally extending axis of the first sheet. The inner packages inthe product loader 124 may contain the same supplies, or the innerpackages may contain different supplies, as desired. For example, aquantity of water-containing inner packages may be supplied to the firstsheet on the first conveyor 116, or the inner packages may alternatinglycontain water, food, and personal hygiene supplies, for example. Incertain embodiments, the packs may be empty and filled at a later timeor place.

The second sheet supply roll 122 continuously provides the materialforming the second sheet for the pack 10. The second sheet may bedistributed from the second sheet supply roll 122 by a pair of overwraprolls and over the inner package and the first sheet, for example. Othersuitable means for distributing the second sheet over the inner packageand the first sheet may also be employed, as desired. The second sheetmay be identical to the first sheet or may be different from the firstsheet.

After the inner package has been disposed between the first and secondsheets, the assembly including the inner package and the first andsecond sheets is advanced to the longitudinal mid-pack and edge sealingunit 104, for example, as illustrated in FIG. 13. The longitudinalmid-pack and edge sealing unit 104 seals the first sheet and the secondsheet to form an outer package housing the inner package. Thelongitudinal mid-pack and edge sealing unit 104 may be a heat sealer,for example, although other means for sealing the inner package betweenthe first and second sheets may also be employed within the scope of thedisclosure.

In a particular embodiment, the longitudinal mid-pack and edge sealingunit 104 heat seals both side edges of the first and second sheets andmid-pack locations of the first and second sheets adjacent the innerpackage. As a nonlimiting example, the longitudinal mid-pack and edgesealing unit 104 may include a pair of side sealing bands 126, 128configured to heat seal the side edges of the first and second sheets.The longitudinal mid-pack and edge sealing unit 104 may also include apair of mid-pack sealing bands 130, 132 configured to heat seal themid-pack areas of the first and second sheets adjacent the innerpackage.

As shown in FIG. 13, the transverse heat sealing unit 106 of the system100 is disposed adjacent the longitudinal mid-pack and edge sealing unit104. At the transverse heat sealing unit 106, top edges and bottom edgesof each of the first and second sheets of the unsealed pack 10 aresealed. The transverse heat sealing unit 106 includes a pair of linearrail mount blocks 134 on which a pair of heat seal cylinders 136 aremovably mounted. The linear rail mount blocks 134 may include bearings,for example, and be biased, for example, with a spring or the like, toreturn to a first location proximal the longitudinal mid-pack and edgesealing unit 104 after being moved to a second location by the firstconveyor 116. The heat seal cylinders 136 selectively actuate an upperheat seal bar 138 and a lower heat seal bar 140.

The partially sealed pack 10 is advanced to the transverse heat sealingunit 106, for example, by the first conveyor 116. The top edges of theof the first and second sheets are first sealed by an actuation of theupper and lower heat seal bars 138, 140 by the heat seal cylinders 136,which causes the upper and lower heat seal bars 138, 140 to compress andheat the first and second sheets therebetween at the first location. Theheat seal cylinders 136 and the upper and lower heat seal bars 138, 140advance with the unsealed pack 10 via coupling the first conveyers,which moves via a positive coupling with the first conveyor, along thelinear rail mount blocks 134. After a predetermined period of time,which time is sufficient to cause the top edges of the first and secondsheets to be sealed, the heat seal cylinders 136 cause the upper andlower heat seal bars 138, 140 to lift from the first and second sheets.The upper and lower heat seal bars 138, 140 are lifted from the firstand second sheets at the second location. The upper and lower heat sealbars 138, 140 are then returned to the first location, and the processrepeated in order to seal the bottom edges of the first and secondsheets. It is understood that the steps that generate the longitudinalmid-pack and edge seals and the top and bottom edge seals may occur in areverse order to that presently described, or may occur substantiallysimultaneously, as desired. In certain embodiments, at least one edge isleft unsealed so that the pack can be filled at a later time or place,after which the remaining edges are sealed.

The transverse heat sealing unit 106 may also be employed to secure atop edge and a bottom edge of the at least one inner package between thefirst sheet and the second sheet with a top transverse seal and a bottomtransverse seal. For example, the upper heat seal bar 138 and the lowerheat seal bar 140 may have raised portions that create each of the topand bottom transverse seals and the top and bottom edge seals. Othermeans for forming the top and bottom transverse seals, to couple theinner package with the outer package, may also be used within the scopeof the present disclosure.

Once the longitudinal mid-pack and edge seals and the transverse top andbottom edge seals are formed, each pack 10 is caused to move past theheat transverse heat sealing unit 106 by the first conveyor 116 to aperforator unit 108. The perforator unit 108 is disposed between thetransverse heat sealing unit 106 and the wing folding unit 110. Theperforator unit 108 transversely perforates the first and second sheetsof the each pack 10 to facilitate separation of the individual packs 10.Additionally, the perforator unit 108 forms a perforation to facilitatean opening of the pack 10.

In a particular embodiment shown in FIG. 14, the perforator unit 108includes a perforation roller 142 with at least one perforation blade144. The perforation roller 142 is disposed opposite an anvil roller146. It should be appreciated that the first conveyor 116 ends adjacentone side of the perforator unit 108, the second conveyor 118 beginsadjacent the other side of the perforator unit 108, and the perforationroller 142 and anvil roller 146 are disposed between the first conveyor116 and the second conveyor 118. The perforation blade 144 of theperforation roller 142 cooperates with the anvil roller to perforate thepacks 10 as they pass therebetween. The perforation blade 144 may have alinear portion for perforating a width of the emergency packs forseparation thereof, and an angular portion for formation of a perforatedopening for the packs 10. The angular portion may be substantiallyV-shaped, for example. The perforation blade 144 may have other shapes,as desired. Other means for perforating the packs 10 may also beemployed within the scope of the present disclosure.

Referring now to FIGS. 15 and 16, the present system 100 furtherincludes a wing folding unit 110 and a wing band sealing unit 112. Thewing folding unit 110 and the wing band sealing unit 112 are configuredto form a pair of aerodynamic elements such as wings on the outerpackage adjacent the at least one inner package. The aerodynamicelements preferably cause turbulent flow across the outer package andreduce or minimize a descent rate of the pack 10 in operation, as thepack 10 is falling through the air. The aerodynamic elements also maycontribute to reducing or minimizing a descent rate of the pack 10 inoperation, as the pack 10 is falling through the air.

As the perforated packs 10 are advanced by the second conveyor 118, thewing folding unit 110 folds a portion of the side edges of the packs 10.For example, the wing folding unit 110 includes a pair of spaced apartfolder bases 146 and a pair of folder guide plates 148 disposed adjacentthe spaced apart folder bases 146. The side edges of the packs 10 areadvanced through the folder guide plates 148, which fold each side edgeto form the drag elements of the packs 10.

Following the folding of the side edges of the packs 10, the folded sideedges are heat sealed with the wing band sealing unit 112, for example,as shown in FIG. 16 Like the longitudinal mid-pack and edge sealing unit104 and the transverse heat sealing unit 106 of the system 100,described hereinabove, the wing band sealing unit 112 is employed toseal the first and second sheets of the packs 10. In particular, thewing band sealing unit 112 may include a pair of heated sealing bands150, 152 that compress and heat the folded edges to form wing seals. Thewing band sealing unit 112 simultaneously forms the drag elements andside sealing edges of the packs 10. It should be understood that theaerodynamic elements or “wings” of the packs 10 are closed as formed,but open in operation, as the pack 10 is falling through the air.

In another embodiment of the present disclosure, rigid inserts may bedisposed adjacent the side edges of the first and second sheets prior toheat sealing by the wing band sealing unit 112. The rigid inserts may beheat sealed into the aerodynamic elements or adjacent the sealing edgesbetween the side edge seals and the mid-pack seals, as desired.

With reference to FIG. 17, the system 100 further may include a packageseparator unit 114. The package separator unit 114 is disposed adjacentthe wing band sealing unit 112, for example. The package separator unit114 may include a guillotine 154. The guillotine 154 is configured tocut along at least a portion of the perforation formed by the perforatorunit 108 and thereby separates each pack 10. The guillotine 154 therebyforms individual ones of the pack 10. As the packs 10 exit the system100, the packs 10 are collected and stored for transport anddistribution. The packs 10 may be collected in a container with noorganization to the packs 10. Alternatively, the packs 10 may becollected in an organized manner resulting in stacked packs 10. Forexample, the container may be a pack magazine containing a desirednumber of packs 10 stacked with the inner package of pack 10 offset fromthe inner package of adjacent packs 10. Other means for collecting theindividual packs 10 may be employed, as desired.

In another embodiment, the individual packs 10 are not separated by thepackage separator unit 114, to provide a linear “string” of packs thatare separated during deployment.

The present disclosure further includes a method for manufacturing thepack 10. The method may be used with the system 100 of the presentdisclosure, or another system, as desired. The method first includes thestep of providing the first sheet and the at least one inner packageincluding the item for aerial delivery. The inner package is thendeposited on the first sheet. A second sheet is disposed over the innerpackage and the first sheet. The first sheet and the second sheet arethen sealed to form the outer package housing the inner package. The atleast one aerodynamic element is formed on the outer package, forexample, adjacent the at least one inner package. The aerodynamicelement preferably causes turbulent flow across the outer package andreduces or minimizes the descent rate of the pack in operation. Theaerodynamic element may also reduces or minimizes the descent rate ofthe pack in operation.

The step of sealing the first sheet and the second sheet may includeforming a top edge seal, a bottom edge seal, and spaced apart side edgeseals on the first sheet and the second sheet. The step of sealing thefirst sheet and the second sheet may also include forming a pair ofmid-pack seals. The inner package is confined within the outer packageby the pair of mid-pack seals, the top edge seal, and the bottom edgeseal.

The step of forming the at least one aerodynamic element may includefolding corresponding side edges of the first sheet and the secondsheet. The folded edges are sealed, for example, between the side edgeseals and the mid-pack seals, to form wing seals.

The inner package may also be coupled to the outer package of the pack10. For example, the top edge and the bottom edge of the at least oneinner package may be sealed between the first sheet and the second sheetwith the top transverse seal and the bottom transverse seal. The innerpackage is thereby coupled to the outer package. Other suitable meansfor coupling the inner package with the outer package, includingadhesives, fasteners, and the like, may also be employed.

The pack 10 of the present disclosure may also be perforated tofacilitate both a separation of the packs 10, and an opening ofindividual packs 10. For example, the perforation may extend inwardlyfrom the top edge of the pack 10. The perforation may traverse at leastone of the top edge seal, the top transverse seal, and the bottomtransverse seal, in order that the seals may be opened. Access to theinner package is thereby permitted.

A method and system for manufacturing a cost-effective pack for suppliesthat may be easily air dropped and distributed to a large number ofpeople, with a minimized risk of damage to the supplies and to thepeople collecting the supplies, is thereby provided.

Other embodiments and uses of the invention will be apparent to thoseskilled in the art from consideration of the specification and practiceof the invention disclosed herein. All references cited herein,including all publications, U.S. and foreign patents and patentapplications, are specifically and entirely incorporated by reference.It is intended that the specification and examples be consideredexemplary only with the true scope and spirit of the invention indicatedby the following claims. Furthermore, the term “comprising” includes theterms “consisting of” and “consisting essentially of,” and the termscomprising, including, and containing are not intended to be limiting.

1. An aerial distribution system for deploying items, comprising: a box;a lid detachably coupled to the box; a plurality of items within thebox; and at least one tether coupling the lid to the box; wherein duringaerial deployment of the aerial distribution system, the lid lifts offfrom the box, remains coupled to the box via the at least on tether, andacts as a canopy to slow the descent of the box.
 2. The aerialdistribution system of claim 1, further comprising a false bottom of thebox, wherein as the lid lifts off from the box, the false bottom isforced through the box and ejects the plurality of items from the box.3. The aerial distribution system of claim 2, wherein the false bottomis coupled to the at least one tether by at least one strap.
 4. Theaerial distribution system of claim 1, wherein the plurality of itemsare aerodynamic supply packs.
 5. The aerial distribution system of claim2, wherein the items are forced out of the bottom of the box.
 6. Theaerial distribution system of claim 2, wherein the box, lid, and falsebottom descend as a single unit.
 7. The aerial distribution system ofclaim 2, wherein the at least one strap is coupled to the false bottomand the box.
 8. (canceled)
 9. (canceled)
 10. (canceled)
 11. (canceled)12. (canceled)
 13. (canceled)
 14. (canceled)
 15. An aerial distributioncontainer, comprising: a box; a lid detachably coupled to the box; andat least one tether coupling the lid to the box; wherein during aerialdeployment of the aerial distribution container, the lid lifts off fromthe box, remains coupled to the box via the at least on tether, and actsas a canopy to slow the descent of the box.
 16. The aerial distributioncontainer of claim 15, further comprising a false bottom of the boxcoupled to the flexible liner, wherein as the lid lifts off from thebox, the false bottom is forced through the box.
 17. The aerialdistribution container of claim 16, wherein the false bottom is coupledto the at least one tether by at least one strap.
 18. The aerialdistribution container of claim 16, wherein the items are forced out ofthe bottom of the box.
 19. The aerial distribution container of claim16, wherein the box, lid, and false bottom descend as a single unit. 20.The aerial distribution container of claim 16, wherein the at least onestrap is coupled to the false bottom and the box.